BACKGROUND OF THE INVENTION
Field of the Invention:
[0001] The present invention relates to a variable-cycle engine which operates in a two-cycle
mode when the rotational speed of the engine is lower than a predetermined speed
and in a four-cycle mode when the rotational speed of the engine is higher than the
predetermined speed.
Description of the Prior Art:
[0002] Ordinary engines are roughly grouped into two-cycle engines in which the intake,
compression, power, and exhaust strokes are performed while the crankshaft makes one
revolution and four-cycle engines in which the above four strokes are carried out
while the crankshaft makes two revolutions.
[0003] In the two-cycle engines, intake ports are positioned in a lower portion of a cylinder
liner. Since intake air is drawn and exhaust gases are discharged when the piston
is lowered, and the explosion occurs each time the crankshaft makes one revolution,
the rotational speed of the output shaft suffers less fluctuations even in a low engine
speed range, and the engine can produce a high-torque output.
[0004] However, since the intake and exhaust strokes are simultaneously performed in the
two-cycle engines, the intake air and the exhaust gases are not fully exchanged particularly
in a high engine speed range. Therefore, the two-cycle engines are lower in efficiency
and higher in fuel consumption.
[0005] In the four-cycle engines, intake air is drawn and exhaust gases are discharged in
respective strokes. Therefore, the intake air and the exhaust gases are well exchanged
in a high engine speed range. Accordingly, the four-cycle engines are highly efficient,
and fuel consumption is lower.
[0006] The four-cycle engines suffer larger fluctuations in the rotational speed of the
engine output shaft. Therefore, in a low engine speed range, the engine output torque
is lower, and the engines do not operate smoothly.
SUMMARY OF THE INVENTION
[0007] In view of the aforesaid problems of the existing engines, it is an object of the
present invention to provide a variable-cycle engine which operates as a two-cycle
engine in an engine speed range lower than a predetermined speed, i.e., a lower engine
speed range, and as a four-cycle engine in an engine speed range higher than the predetermined
speed, i.e., a higher engine speed range.
[0008] To achieve the above object, there is provided in accordance with the present invention
a variable-cycle engine selectively operable in different cycle modes depending on
the rotational speed thereof, comprising a cylinder having a first intake port and
an exhaust port which are defined in an upper portion thereof, a piston reciprocally
fitted in the cylinder and having a piston head surface, the cylinder also having
a second intake port defined in a cylindrical wall thereof and positioned such that
the second intake port corresponds in position to the piston head surface when the
piston is positioned near the bottom dead center thereof, an intake valve for opening
and closing the first intake port, an exhaust valve for opening and closing the exhaust
port, a sleeve valve slidably fitted over the cylinder and angularly movable around
the cylinder, for opening and closing the second intake port, intake valve actuator
means for actuating the intake valve to open and close the first intake port, exhaust
valve actuator means for actuating the exhaust valve to open and close the exhaust
port, sleeve valve actuator means for angularly moving the sleeve valve to open and
close the second intake port, supercharging means for supplying intake air under pressure
through at least the second intake port into the cylinder, two fuel injection nozzles
alternately operable to inject fuel into the cylinder each time the engine makes one
revolution, injection timing varying means for inactivating one of the two fuel injection
nozzles, and cycle mode selecting means for detecting the rotational speed of the
engine, and for activating the exhaust valve actuator means, inactivating the intake
valve actuator means and the injection timing varying means, and activating the sleeve
valve actuator means to open the second intake port, thereby operating the engine
in a two-cycle mode, when the detected rotational speed is lower than a predetermined
speed, and for activating the intake valve actuator means, the exhaust valve actuator
means, and the injection timing varying means, and inactivating the sleeve valve actuator
means to close the second intake port, thereby operating the engine in a four-cycle
mode, when the detected rotational speed is higher than the predetermined speed.
[0009] According to the present invention, there is also provided a variable-cycle engine
selectively operable in different cycle modes depending on the rotational speed thereof,
comprising a cylinder having an exhaust port which is defined in an upper portion
thereof, an exhaust valve for opening and closing the exhaust port, valve actuator
means for actuating the exhaust valve to open and close the exhaust port, a piston
reciprocally fitted in the cylinder and having a piston head surface, the cylinder
also having an intake port defined in a cylindrical wall thereof and positioned such
that the intake port corresponds in position to the piston head surface when the piston
is positioned near the bottom dead center thereof, supercharging means for supplying
intake air under pressure from the intake port into the cylinder, two fuel injection
nozzles alternately operable to inject fuel into the cylinder each time the engine
makes one revolution, injection timing varying means for inactivating one of the two
fuel injection nozzles, and cycle mode selecting means for detecting the rotational
speed of the engine, and for activating the exhaust valve actuator means to operate
the exhaust valve each time the engine makes one revolution, and inactivating the
injection timing varying means, thereby operating the engine in a two-cycle mode,
when the detected rotational speed is lower than a predetermined speed, and for activating
the exhaust valve actuator means to operate the exhaust valve each time the engine
makes two revolutions, and activating the injection timing varying means, thereby
operating the engine in a four-cycle mode, when the detected rotational speed is higher
than the predetermined speed.
[0010] In a lower engine speed range, the engine operates as a two-cycle engine, and hence
the engine rotates smoothly and produces high output torque. In a higher engine speed
range, the engine operates as a four-cycle engine, and thus consumes less fuel and
operates highly efficiently.
[0011] If the variable-cycle engine operates as a power unit for motor vehicles, then the
number of gear positions of a transmission combined with the engine may be reduced
or eliminated.
[0012] Furthermore, when the rotational speed of the engine is low, depending on the load
on the engine, a reduction in the boost pressure due to a shortage of the exhaust
energy is compensated for by energizing a rotary electric machine mounted on the shaft
of a supercharging means, thereby to assisting in rotating the compressor of the supercharging
means. Therefore, the boost pressure is increased to enable the engine to produce
high output torque when the engine speed is low and the load on the engine is large.
[0013] The above and other objects, features and advantages of the present invention will
become more apparent from the following description when taken in conjunction with
the accompanying drawings in which preferred embodiments of the present invention
are shown by way of illustrative example.
BRIEF DESCRIPTION OF THE DRAWINGS
[0014]
Fig. 1 is a cross-sectional view, partly in block form, of a variable-cycle engine
according to a first embodiment of the present invention;
Fig. 2 is a cross-sectional view taken along line II - II of Fig. 1;
Fig. 3 is a cross-sectional view of a valve actuator;
Fig. 4 is a cross-sectional view, partly in block form, of a variable-cycle engine
according to a second embodiment of the present invention;
Fig. 5 is a cross-sectional view taken along line V - V of Fig. 4;
Fig. 6 is a cross-sectional view taken along line VI - VI of Fig. 4;
Fig. 7 is a graph showing a pressure vs. volume (p - v) diagram of the engine shown
in Fig. 4 when it operates in a four-cycle mode;
Fig. 8 is a diagram showing certain strokes of the engine shown in Fig. 4 when it
operates in the four-cycle mode;
Figs. 9(a) and 9(b) show an injection timing varying device; and
Fig. 10 is a graph showing the relationship between rotational speeds and torques.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0015] A variable-cycle engine according to a first embodiment of the present invention
will be described with reference to Figs. 1 through 3.
[0016] As shown in Figs. 1 and 2, a cylinder liner 11 is fitted against the inner wall of
a cylinder 1. A piston 2 is reciprocally fitted in the cylinder 1. The cylinder liner
11 has a circumferential array of intake ports 12 defined in its peripheral wall.
The intake ports 12 are positioned such that they are near the upper end of a piston
head 21 of the piston 2 when the piston 2 reaches the bottom dead center.
[0017] The intake ports 12 are inclined with respect to the central axis of the cylinder
1 for introducing intake air from an intake pipe 13 as a swirling flow into the cylinder
1.
[0018] A sleeve valve 3 in the form of an annular strip is fitted over the cylinder liner
11 in covering relation to the openings of the intake ports 12. The sleeve valve 3
is circumferentially slidable on and about the cylinder liner 11. The sleeve valve
3 has holes 31 defined therein and corresponding in position to the intake ports 12.
When the sleeve valve 3 is angularly moved circumferentially around the cylinder 1,
the intake ports 12 are covered with those portions of the sleeve valve 3 which lie
between the holes 31, thereby preventing intake air from passing through the intake
ports 12. The sleeve valve 3 has a number of gear teeth 32 disposed on and along a
lower edge thereof and projecting radially outwardly.
[0019] The sleeve valve 3 is actuatable by a sleeve valve actuator 4 which has a gear 41
held in mesh with the gear teeth 32 of the sleeve valve 3. When the sleeve valve actuator
4 is operated, it enables the gear 41 and the gear teeth 32 meshing therewith to turn
the sleeve valve 3 through a predetermined angle. The sleeve valve actuator 4 is operable
by a command signal from a controller 8 (described later on).
[0020] An intake valve 16 is disposed upwardly of the cylinder 1, for introducing intake
air from an intake pipe 14 into the cylinder 1 depending on operation of the engine.
The intake valve 16 can be opened and closed by an electromagnetic valve actuator
5 disposed above the intake valve 16.
[0021] An exhaust valve 17 is also disposed upwardly of the cylinder 1 adjacent to the intake
valve 16, for discharging exhaust gases into an exhaust pipe 15 in an exhaust stroke
of the engine. The exhaust valve 17 can be opened and closed by an electromagnetic
valve actuator 6 disposed above the exhaust valve 17.
[0022] The electromagnetic valve actuators 5, 6 are identical in structure to each other.
Only the electromagnetic valve actuator 6 will be described below by way of example
with reference to Fig. 3.
[0023] Two permanent magnets 61, 62 are fitted over the end of the shank of the exhaust
valve 17 in axially spaced relationship. The permanent magnets 61, 62 have respective
outer peripheral portions which are magnetized in different polarities. For example,
if the outer peripheral portion of the permanent magnet 61 is of N pole, then the
outer peripheral portion of the permanent magnet 62 is of S pole.
[0024] Magnetic poles 63 are disposed in confronting relation to the permanent magnets
61, 62 and juxtaposed in the direction in which the exhaust valve 17 is movable. The
magnetic poles 63 are spaced by intervals different from the interval by which the
permanent magnets 61, 62 are spaced from each other. Coils 64 for controlled the polarity
of the magnetic poles 63 are wound around the respective magnetic poles 63.
[0025] The coils 64 are energized under the control of the controller 8 such that the polarities
of the magnetic poles 63 confronting the permanent magnets 61, 62 are successively
varied. The electromagnetic forces thus acting between the permanent magnets 61, 62
and the magnetic poles 63 are combined to move the exhaust valve 17 in opening and
closing directions.
[0026] A turbocharger 7 comprises a turbine 71, a rotary electric machine 72, and a compressor
73 which are arranged in coaxial relationship. When the turbine 71 is driven by the
energy of exhaust gases discharged from the discharge pipe 15, the compressor 73 is
rotated to supply air under pressure to the cylinder 1 through an intake pipe 13 communicating
with the sleeve valve 3 and the intake pipe 14.
[0027] Depending on the operating condition of the engine, the rotary electric machine 72
is supplied with electric energy and hence operates as a motor to assist in rotating
the compressor 73 for increasing the engine torque in a low engine speed range.
[0028] The rotational speed of the crankshaft of the engine is detected by an engine rotation
sensor 81 for the detection of the rotational speed of the engine. The amount of fuel
supplied to the engine is detected by an engine load sensor for the detection of the
load on the engine. The crankshaft angle is detected by a position sensor 83 for the
detection of the position of the piston. Detected signals from these sensors are applied
to the controller 8.
[0029] Injection nozzles 91, 92 are mounted on an upper portion of the cylinder 1, for injecting
fuel into the cyl inder 1 in a direction along intake air swirls. The injection
nozzles 91, 92 are connected to a fuel pump 93 by which the timing to inject fuel
and the amount of fuel to be injection can be varied.
[0030] The controller 8 comprises a microcomputer having a central processing unit for effecting
arithmetic operations, various memories for storing sequences for the arithmetic operations
and a control sequence, and input/output ports. When the signals from the sensors
are supplied to the controller 8, the predetermines arithmetic operations are carried
out, and control signals are transmitted to the sleeve valve actuator 4, the electromagnetic
valve actuators 5, 6, the rotary electric machine 72, and the fuel pump 93 according
to the stored control sequence.
[0031] The variable-cycle engine according to the first embodiment operates as follows:
[0032] In an engine speed range in which the rotational speed indicated by the detected
signal from the rotation sensor 81 is lower than a predetermined speed, the controller
8 applies a control signal to the sleeve valve actuator 4 to bring the holes 31 of
the sleeve valve 3 into registry with the intake ports 12 of the cylinder liner 11,
so that the engine will operate in a two-cycle mode. Therefore, the sleeve valve 3
is angularly positioned as shown in Figs. 1 and 2.
[0033] When the piston 2 is lowered toward the bottom dead center, intake air supplied under
pressure from the turbocharger 7 through the intake pipe 13 flows as swirling air
into the cylinder 1 through the holes 31 and the intake ports 12 which are aligned
with each other. The introduced swirling air forces the exhaust gases out of the cylinder
1 through the opened exhaust port 15, and is available as intake air which is needed
in the next combustion stroke.
[0034] Then, the piston 2 moves upwardly, closing the intake ports 12 of the cylinder liner
11. Soon thereafter, the exhaust valve 17 is closed, and the volume of the cylinder
1 is compressed. At a final stage of the compression stroke, the temperature in the
cylinder 1 rises to the point where fuel can be ignited. Then the injection nozzle
91 or 92 injects fuel into the cylinder 1. The injected fuel is ignited and combusted,
whereupon the piston 2 is lowered under high combustion pressure for thereby rotating
the crankshaft.
[0035] In the latter half of the expansion stroke, the exhaust valve 17 is opened, and the
combustion gases are discharged under their own pressure through the exhaust pipe
15 to the turbocharger 7. The exhaust gases rotate the turbine 71 and are then discharged
from the turbocharger 7.
[0036] Upon further descent of the piston 2, the gas pressure in the cylinder 1 sufficiently
lowered. When the upper end of the piston 2 reaches the intake ports 12, intake air
is supplied again under pressure from the turbocharger 7 into the cylinder 1 through
the intake ports 12, scavenging any remaining exhaust gases from the cylinder 1. At
this time, any resistance to the influx of intake air is small and the intake air
can be introduced into the cylinder 1 in a short period of time since the intake ports
12 are arrayed fully circumferentially in the lower portion of the cylinder liner
11 and held in communication with the holes 31 of the sleeve valve 3.
[0037] In an engine speed range in which the rotational speed indicated by the detected
signal from the rotation sensor 81 is higher than a predetermined speed, the engine
operates in a four-cycle mode.
[0038] In this mode, the controller 8 controls the electromagnetic valve actuator 5 and
the sleeve valve actuator 4 such that the intake valve 16 is opened and closed by
the electromagnetic valve actuator 5 in the intake stroke of an ordinary four-cycle
engine and the intake ports 12 of the cylinder liner 11 are closed by the sleeve valve
3.
[0039] When the piston 2 is lowered, since the intake ports 12 of the cylinder liner 11
are closed by the sleeve valve 3, the combustion gases are prevented from flowing
into the intake ports 12. In the intake stroke, sufficient intake air is introduced
from the upper intake valve 16. As the lower volume of the cylinder 1 is not made
a dead volume, the stroke of the piston can effectively be utilized.
[0040] A variable-cycle engine according to a second embodiment will be described below
with reference to Figs. 4, 5, and 6.
[0041] A cylinder sleeve 110 is fitted against the inner wall of a cylinder 100. A piston
300 is reciprocally fitted in the cylinder 100. The cylinder sleeve 110 has a circumferential
array of intake ports 130 defined in its peripheral wall. The intake ports 130 are
positioned such that they are near the upper end of a piston head of the piston 300
when the piston 300 reaches the bottom dead center. The intake ports 130 are inclined
with respect to the central axis of the cylinder 100 for introducing swirling intake
air into the cylinder 100.
[0042] The engine has a prechamber 200 defined centrally in a portion above the cylinder
100 and having an inner wall covered with a sleeve 210 which is made of a heat-resistant
heat insulating material such as ceramic. The sleeve 210 and the cylinder sleeve 110
are connected to each other through a heat insulating gasket 120.
[0043] Injection nozzles 220, 250 are disposed laterally of the prechamber 200, for injecting
fuel into the prechamber 200 along swirls in the prechamber 200 (see Fig. 5). The
injection nozzles 220, 250 are connected to a fuel pump 230 by which the timing to
inject fuel and the amount of fuel to be injection can be varied. The prechamber 200
has an exhaust port for discharging exhaust gases through the prechamber 200. The
exhaust port can be opened and closed by an exhaust valve 240, which is axially movable
by a valve actuator 600 disposed around the shank of the exhaust valve 240.
[0044] The valve actuator 600 is structurally identical to the electromagnetic valve actuator
6 according to the first embodiment of the present invention.
[0045] The piston head surface of the piston 300 disposed in the cylinder 100 is covered
with a heat-resistant heat insulating material such as ceramic, as with the prechamber
200. The piston 300 has a projection 310 a projection extending from the center of
the piston head toward the prechamber 200. When the piston 300 reaches a position
near the top dead center of its stroke, the projection 310 narrows the opening of
the prechamber 200.
[0046] Exhaust gases discharged from the exhaust port are led through an exhaust pipe 410
to the turbine of a turbocharger 400. The turbocharger 400 has a rotatable shaft
to which a rotary electric machine 430 is connected. When the rotary electric machine
is energized by electric power supplied from an external power supply, it can develop
a boost pressure.
[0047] The exhaust gases which have gone past the turbocharger 400 are led to a recovery
turbine 440 by which remaining heat energy of the exhaust gases is converted into
electric energy which is recovered by a controller 500.
[0048] The compressor of the turbocharger 400 can be rotated by the energy of the exhaust
gases applied to the turbine or the electric energy supplied to the rotary electric
machine, for supplying intake air under boost pressure through an intake pipe 420
to the intake ports 130.
[0049] The valve actuator 600, the fuel pump 230, and the rotary electric machine 430 are
controlled by signals supplied from an input/output interface of the controller 500.
To the input/output interface, there are connected a rotation sensor 550 for detecting
the rotational speed and crankshaft angle fo the engine, and an accelerator pedal
movement sensor 560 for detecting the amount of depression of the accelerator pedal
associated with the engine, and an electric generator of the recovery turbine 440.
Therefore, signals from these sensors and recovered electric energy are applied to
the controller 500.
[0050] The control unit 500 is of the same construction as that of the controller 8 according
to the first embodiment.
[0051] A two-cycle mode in which the engine of the second embodiment operates as a two-cycle
engine will be described below.
[0052] When the expansion stroke ends and the piston 300 is positioned near the bottom dead
center, intake air supplied under boost pressure from the intake ports 130 flows
into the cylinder 100 in which the intake air flows as circumferential air swirls.
As the piston 300 moves upwardly, it pushes the exhaust gases upwardly and scavenges
the exhaust gases from the exhaust port. On the upward movement of the piston 300,
the exhaust port is closed by the exhaust valve 240, and the piston 300 enters the
compression stroke in which the intake air is compressed. The continued ascent of
the piston 300 accelerates the intake air in the cylinder 100 and forces the intake
air into the prechamber 200.
[0053] When fuel is injected from the injection nozzles 200 into the prechamber 200 along
the air swirls therein, the fuel is combusted. The piston 300 now enters the expansion
stroke. The injected fuel is fully combusted in the prechamber 200 and the produced
exhaust gases lower the piston 300. When the piston 300 is lowered, the opening of
the prechamber 200 which has been narrowed by the projection 310 is enlarged, allowing
the exhaust gases to be spread quickly into the cylinder 100. On the downward movement
of the piston 300, the exhaust valve 240 is actuated to open the exhaust port for
thereby discharging the exhaust gases. The above cycle is repeated following the next
intake stroke.
[0054] A four-cycle mode in which the engine operates as a four-cycle engine will now be
described below with reference to Figs. 7 and 8. Engine conditions at points
a through
e in Fig. 7 are shown at
a through
e, respectively, in Fig. 8.
[0055] When the volume of the cylinder 100 and the prechamber 200 is increased from a point
V1 at the top dead center where the combustion chamber is compressed to a point V2
immediately prior to the bottom dead center, in the expansion stroke after combustion,
the exhaust port is opened to start discharging the exhaust gases.
[0056] While the volume is expanded through a condition shown at
a in Fig. 8 to a point V3 at the bottom dead center, the pressure in the cylinder 100
and the prechamber 200 quickly drops. Since the intake ports 130 are opened at the
bottom dead center shown at
b in Fig. 8, intake air supplied under boost pressure is introduced as swirling air
flows into the cylinder 100.
[0057] The introduced intake air pushes the exhaust gases upwardly to assist in discharging
the exhaust gases from the exhaust port. The piston 300 moves upwardly from the bottom
dead center, closing the intake ports 130 to stop introducing the intake air. Even
at this time, exhaust gases still remain in the cylinder 100. Therefore, the exhaust
port remains open as indicated at
c in Fig. 8. The exhaust port is continuously open until the piston 300 reaches the
top dead center, whereupon the exhaust gases are completely discharged from the cylinder.
[0058] Then, the exhaust port is closed at the top dead center V1 as indicated at
d in Fig. 8. With the exhaust port closed, the piston 300 is lowered to cause the intake
air sealed in the cylinder 100 to be adiabatically expanded. Since the temperature
of the intake air is lowered during the adiabatic expansion, the intake air quickly
absorbs heat energy from the inner wall of the combustion chamber, thus lowering the
temperature of the combustion chamber inner wall.
[0059] When the piston 300 moves past a point immediately prior to the bottom dead center
V3 as indicated at
e in Fig. 8, intake air rapidly flows from the intake ports 130 into the cylinder 100
under the boost pressure and a vacuum developed in the cylinder 100. Since the intake
ports 130 are inclined with respect to the central axis of the cylinder 100 as shown
Fig. 6, the introduced intake air swirls at high speed in the cylinder 100.
[0060] As the piston 300 moves upwardly, the swirling air flows in the cylinder 100 are
moved into the prechamber 200.
[0061] In the latter half of the compression stroke of the piston 300, the amount of intake
air flowing into the prechamber 200 is reduced. However, the projection 310 on the
piston head enters narrows the opening of the prechamber 200, thereby accelerating
the air swirls as they go into the prechamber 200. Accordingly, when the compression
stroke ends, air swirls at higher speed are produced in the prechamber 200. Then,
fuel is injected from the injection nozzle 220 into the prechamber 200 along the air
swirls. The injected is fuel is now ignited and combusted, and then the piston 300
initiates the expansion stroke.
[0062] An injection timing varying means which includes the fuel pump 230 will be described
below with reference to Fig. 9. The engine according to the first embodiment also
has an injection timing varying means which includes the fuel pump 92, the injection
timing varying means being identical to the injection timing varying means shown
in Fig. 9.
[0063] Fig. 9(a) shows in block form the injection timing varying means. Fig. 9(a) is a
combination of the view taken along line V - V of Fig. 4 and a view showing a structure
of the fuel pump 230.
[0064] The injection nozzle 220 is angularly oriented to inject fuel along the wall surface
of the prechamber 200 along which the air swirls flow. The injection nozzle 250 is
angularly oriented to inject fuel more toward the center of the prechamber 200 than
the injection nozzle 220.
[0065] The injection nozzle 220 is coupled to a plunger pump 710 which is actuated by a
cam A, and the injection nozzle 220 is coupled through a directional control valve
730 to a plunger pump 720 which is actuated by a cam B.
[0066] Fig. 9(b) illustrates the cam profiles of the cams A, B. The cams A, B operate the
pump plungers 710, 720, respectively, each time the engine makes one revolution, but
out of phase by one revolution.
[0067] When the engine operates as a four-cycle engine, the supply of fuel to the injection
nozzle 250 is cut off by the directional control valve 730, so that fuel is supplied
from only the injection nozzle 220. Since the rotational speed of the engine is high
when the engine operates as a four-cycle engine, the air swirls at a high speed in
the prechamber 200, and the fuel which is injected along the prechamber wall from
the injection nozzle 220 is well combusted.
[0068] When the rotational speed of the engine is lower than a predetermined speed, the
directional control valve 730 is opened to supply fuel to the injection nozzle 250.
Fuel is now injected alternately from the injection nozzles 220, 250 each time the
engine makes one revolution. Since the injection nozzle 250 injects fuel more toward
the center of the prechamber 200 than the injection nozzle 220, the fuel injected
from the injection nozzles 220, 250 is shifted as a whole toward the center of the
prechamber 200. Therefore, fuel can also be well combusted in the lower speed range
in which the air swirls at a lower speed.
[0069] The relationship between the rotational speeds and torques of the engines according
to the first and second embodiments of the present invention will be described with
reference to Fig. 10.
[0070] The graph of Fig. 10 has a horizontal axis representing the rotational speed N of
the engine, and a vertical axis representing the torque T produced by the engine.
[0071] In a range in which the rotational speed N is higher than a predetermined speed N2,
the engine operates as a four-cycle engine. In a range in which the rotational speed
N is lower than the predetermined speed N2, the engine operates as a two-cycle engine.
[0072] In a range in which the rotational speed N is lower than a lower speed N1, since
the energy of exhaust gases is insufficient, electric energy is supplied to the rotary
electric machine 72 or 430 for increasing the boost pressure under which intake air
is supplied to the cylinder. In this manner, the torque of the engine is increased
in such a lower speed range.
[0073] If the load on the engine is increased in the speed ranges higher than the speed
N1, then electric power is supplied to the rotary electric machine 72 or 430 to increase
the boost pressure, and the amount of injected fuel is also increased, for thereby
increasing the output power of the engine.
[0074] If the engine is operated in the manner described above, the torque generated by
the engine increases as the rotational speed decreases. The engine thus controlled
is optimum for use as a power unit for motor vehicles. An advantage of the engine
with such torque characteristics is that the number of gear positions of a transmission
combined with the engine may be reduced or such gear positions may be eliminated.
[0075] Although certain preferred embodiments have been shown and described, it should be
understood that many changes and modifications may be made therein without departing
from the scope of the appended claims.
1. A variable-cycle engine selectively operable in different cycle modes depending
on the rotational speed thereof, comprising:
a cylinder having a first intake port and an exhaust port which are defined in an
upper portion thereof;
a piston reciprocally fitted in said cylinder and having a piston head surface, said
cylinder also having a second intake port defined in a cylindrical wall thereof and
positioned such that the second intake port corresponds in position to the piston
head surface when said piston is positioned near the bottom dead center thereof;
an intake valve for opening and closing said first intake port;
an exhaust valve for opening and closing said exhaust port;
a sleeve valve slidably fitted over said cylinder and angularly movable around said
cylinder, for opening and closing said second intake port;
intake valve actuator means for actuating said intake valve to open and close said
first intake port;
exhaust valve actuator means for actuating said exhaust valve to open and close said
exhaust port;
sleeve valve actuator means for angularly moving said sleeve valve to open and close
said second intake port;
supercharging means for supplying intake air under pressure through at least said
second intake port into said cylinder;
two fuel injection nozzles alternately operable to inject fuel into said cylinder
each time the engine makes one revolution;
injection timing varying means for inactivating one of said two fuel injection nozzles;
and
cycle mode selecting means for detecting the rotational speed of the engine, and
for activating said exhaust valve actuator means, inactivating said intake valve actuator
means and said injection timing varying means, and activating said sleeve valve actuator
means to open said second intake port, thereby operating the engine in a two-cycle
mode, when the detected rotational speed is lower than a predetermined speed, and
for activating said intake valve actuator means, said exhaust valve actuator means,
and said injection timing varying means, and inactivating said sleeve valve actuator
means to close said second intake port, thereby operating the engine in a four-cycle
mode, when the detected rotational speed is higher than said predetermined speed.
2. A variable-cycle engine according to claim 1, wherein said supercharging means
comprises a turbocharger having a compressor drivable by the energy of exhaust gases
discharged from said exhaust port, for supplying intake air under pressure, and a
rotary electric machine for assisting in driving said compressor.
3. A variable-cycle engine according to claim 2, further comprising supercharging
assisting means for energizing said rotary electric machine to assist in driving
said compressor when the rotational speed is lower than another predetermined speed
lower than said first-mentioned predetermined speed.
4. A variable-cycle engine according to claim 1, wherein said sleeve valve comprises
an annular strip extending around said cylinder and slidably circumferentially for
opening and closing said second intake port.
5. A variable-cycle engine according to claim 1, wherein said second intake port is
inclined with respect to the central axis of said cylinder, said one of the fuel injection
nozzles which is inactivated by said injection timing varying means being oriented
to inject fuel along a swirling flow of intake air which is drawn into said cylinder
from said second intake port, the other fuel injection nozzle being oriented to inject
fuel along the swirling flow and also more along an inner wall surface of said cylinder
than said one fuel injection valve.
6. A variable-cycle engine selectively operable in different cycle modes depending
on the rotational speed thereof, comprising:
a cylinder having an exhaust port which is defined in an upper portion thereof;
an exhaust valve for opening and closing said exhaust port;
valve actuator means for actuating said exhaust valve to open and close said exhaust
port;
a piston reciprocally fitted in said cylinder and having a piston head surface, said
cylinder also having an intake port defined in a cylindrical wall thereof and positioned
such that the intake port corresponds in position to the piston head surface when
said piston is positioned near the bottom dead center thereof;
supercharging means for supplying intake air under pressure from said intake port
into said cylinder;
two fuel injection nozzles alternately operable to inject fuel into said cylinder
each time the engine makes one revolution;
injection timing varying means for inactivating one of said two fuel injection nozzles;
and
cycle mode selecting means for detecting the rotational speed of the engine, and
for activating said exhaust valve actuator means to operate said exhaust valve each
time the engine makes one revolution, and inactivating said injection timing varying
means, thereby operating the engine in a two-cycle mode, when the detected rotational
speed is lower than a predetermined speed, and for activating said exhaust valve
actuator means to operate said exhaust valve each time the engine makes two revolutions,
and activating said injection timing varying means, thereby operating the engine in
a four-cycle mode, when the detected rotational speed is higher than said predetermined
speed.
7. A variable-cycle engine according to claim 6, wherein said supercharging means
comprises a turbocharger having a compressor drivable by the energy of exhaust gases
discharged from said exhaust port, for supplying intake air under pressure, and a
rotary electric machine for assisting in driving said compressor.
8. A variable-cycle engine according to claim 7, further comprising supercharging
assisting means for energizing said rotary electric machine to assist in driving
said compressor when the rotational speed is lower than another predetermined speed
lower than said first-mentioned predetermined speed.
9. A variable-cycle engine according to claim 6, wherein said intake port is inclined
with respect to the central axis of said cylinder, said one of the fuel injec tion
nozzles which is inactivated by said injection timing varying means being oriented
to inject fuel along a swirling flow of intake air which is drawn into said cylinder
from said intake port, the other fuel injection nozzle being oriented to inject fuel
along the swirling flow and also more along an inner wall surface of said cylinder
than said one fuel injection valve.